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  • 标题:Hybrid Rocket Technology
  • 本地全文:下载
  • 作者:Sankaran Venugopal ; K K Rajesh ; V Ramanujachari
  • 期刊名称:Defence Science Journal
  • 印刷版ISSN:0976-464X
  • 出版年度:2011
  • 卷号:61
  • 期号:3
  • 页码:193-200
  • DOI:10.14429/dsj.61.518
  • 语种:English
  • 出版社:Defence Scientific Information & Documentation Centre
  • 摘要:With their unique operational characteristics, hybrid rockets can potentially provide safer, lower-cost avenues for spacecraft and missiles than the current solid propellant and liquid propellant systems. Classical hybrids can be throttled for thrust tailoring, perform in-flight motor shutdown and restart. In classical hybrids, the fuel is stored in the form of a solid grain, requiring only half the feed system hardware of liquid bipropellant engines. The commonly used fuels are benign, nontoxic, and not hazardous to store and transport. Solid fuel grains are not highly susceptible to cracks, imperfections, and environmental temperature and are therefore safer to manufacture, store, transport, and use for launch. The status of development based on the experience of the last few decades indicating the maturity of the hybrid rocket technology is given in brief. Defence Science Journal, 2011, 61(3), pp.193-200 , DOI:http://dx.doi.org/10.14429/dsj.61.518
  • 关键词:MECHANICAL ENGG./AEROSPACE ENGG.
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